DocumentCode :
841673
Title :
On the feasibility of real-time prediction of aircraft carrier motion at sea
Author :
Sidar, Menahem M. ; Doolin, Brian F.
Author_Institution :
NASA, Moffett Field, CA, USA
Volume :
28
Issue :
3
fYear :
1983
fDate :
3/1/1983 12:00:00 AM
Firstpage :
350
Lastpage :
356
Abstract :
Landing aircraft on board carriers is a most delicate phase of flight operations at sea. The ability to predict the aircraft carrier´s motion over an interval of several seconds within reasonable error bounds may allow an improvement in touchdown dispersion and reduce the value of the ramp clearance due to a smoother aircraft trajectory. Also, improved information to the landing signal officer should decrease the number of waveoffs substantially. This paper indicates and shows quantitatively that, based upon the power density spectrum data for pitch and heave measured for various ships and sea conditions, the motion can be predicted well for up to 15 s. Moreover, the zero crossover times for both pitch and heave motions can be predicted with impressive accuracy. The predictor was designed on the basis of Kalman´s optimum filtering theory (the discrete time case), being compatible with real-time digital computer operation.
Keywords :
Aircraft landing guidance; Kalman filtering, linear systems; Marine-vehicle control; Motion measurements; Prediction methods; Accuracy; Aircraft; Density measurement; Filtering theory; Kalman filters; Marine vehicles; Motion measurement; Power measurement; Sea measurements; Trajectory;
fLanguage :
English
Journal_Title :
Automatic Control, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9286
Type :
jour
DOI :
10.1109/TAC.1983.1103227
Filename :
1103227
Link To Document :
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